# Service difficulty reports: N587JB

A list on [N587JB](https://openairdocs.org/aircraft/N587JB.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 106 reports

- [SDR YENA2026020400142](https://openairdocs.org/sdr/YENA2026020400142.md): Panel · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Keel
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AT KEEL BEAM BOTTOM PANEL FASTENER HOLES 5, CRACK DEPTH 0.105 INCHES FWD DIRECTION; REF AEROMAN NR 2025-682674 WO 2025 413/1 ACCOMPLISHED REPAIR OF CRACK DAMAGE ON HOLE #5 ON THE CENTER FUSELAGE KEEL BEAM BOTTOM
- [SDR YENA2026020400141](https://openairdocs.org/sdr/YENA2026020400141.md): Window Frame · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER OPOST LOWER ATTACHMENT, VERTICAL FLANGE AREA RH SIDE. CRACK LENGTH 0.196 INCHES APPROX; REF AEROMAN NR 2025-682430 WO 2025 413/1 ERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAME CENT
- [SDR YENA2026020400140](https://openairdocs.org/sdr/YENA2026020400140.md): Frame · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FR 36 IN FASTENER HOLE LOC Y1292 MORE 2 INCH UPPER SURFACE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX CRACK AT 12 O'CLOCK CRACK DEPTH 0.157 INCH APPROX IN FWD CARGO COMPARTMENT; PERFORMED REPAIR IAW EC A26-01
- [SDR YENA2026020400139](https://openairdocs.org/sdr/YENA2026020400139.md): Frame · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN OPEN HOLE FASTENER LOC Y1292 MORE 4 INCH UPPER SURFACE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX CRACK AT 5 O'CLOCK, CRACK DEPTH 0.160 INCH APPROX IN FWD CARGO COMPARTMENT (1 EA); PERFORMED REPAI
- [SDR YENA2026020400138](https://openairdocs.org/sdr/YENA2026020400138.md): Frame · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN OPEN HOLE FASTENER LOCATION Y1292 MORE 5 INCH UPPER SURFACE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX CRACK AT 6 O'CLOCK POSITION, CRACK DEPTH 0.131 INCH APPROX IN FWD CARGO COMPARTMENT (1EA); PE
- [SDR YENA2026020400137](https://openairdocs.org/sdr/YENA2026020400137.md): Frame · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FR 36 IN OPEN FASTENER LHOLE LOC Y1292 MORE 8 INCH UPPER SURFACE OF THE PRESSURE DECK MEMBRANE TO CNETER WING BOX. CRACK AT 1 O'CLOCK CRACK DEPTH 0,140 INCH APPROX IN FWD CARGO COMPARTMENT (1 EA); REF AEROMAN NR 2
- [SDR YENA2026020400136](https://openairdocs.org/sdr/YENA2026020400136.md): Fitting · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK ON CONTINUITY FITTING LH AT COCKPIT; REF AEROMAN NR 2025-682704 WO 2025 413/1 PERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAME CENTER POST LOWER NODE AREA R/H VERTICAL FLANGE AND CONTINUITY FITTINGS ASPER AEROMAN EA# 53
- [SDR YENA2026020400135](https://openairdocs.org/sdr/YENA2026020400135.md): Structure · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 1, POSITION 4 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FR 36, CRACK DEPTH 0.129 INCH CRACK DIRECTION 3 AND 4 O'CLOCK VIEW LOOKING AFT; REF AEROMAN NR 2025-682309 WO 2025 413/1 PERFORME
- [SDR YENA2026020400134](https://openairdocs.org/sdr/YENA2026020400134.md): Stringer · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 1 POSITION 6 OF VERTICAL STRINGER REDIUS IN CNETER FUSELAGE ON FRAME 36 CRACK DEPTH O.085 INCH CRACK DIRECTION 6 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC NO. A25-1157-01 AND EA NO. 57-
- [SDR YENA2026020400133](https://openairdocs.org/sdr/YENA2026020400133.md): Stringer · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE W1, POSITION 1 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FRAME 36 CRACK DEPTH 0.100 INCH CRACK DIRECTION 12 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC A25-1157-01 AND EA 57-117-
- [SDR YEN2026F00001](https://openairdocs.org/sdr/YEN2026F00001.md): Stringer · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 2, POSITION 2 OF VERTICAL STRINGER RADIUS IN CENTER FUSELGAE ON FRAME 36, CRACK DEPTH 0.130 INCH. CRACK DIRECTION 8 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC A25-1157-01 AND EA 57-0017-
- [SDR YENA2026020400131](https://openairdocs.org/sdr/YENA2026020400131.md): Stringer · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 2, POSITION 5 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.127 INCH, CRACK DIRECTION 8 AND 9 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC A25-1157-01 AND EA 5
- [SDR YENA2026020400132](https://openairdocs.org/sdr/YENA2026020400132.md): Stringer · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLDE ZONE 2, POSITION 5 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.127 INCH CRACK DIRECTION 8 AND 9 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC NO. A25-1157-01 AND
- [SDR YENA2026020400130](https://openairdocs.org/sdr/YENA2026020400130.md): Stringer · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 2, POSITION 5 OF VERTICAL STRINGER RADIUS IN CNETER FUSELAGE ON FRAME 36. CRACK DEPTH 0.127 INCH, CRACK DIRECTION 8 AND 9 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC A25-1157-01 AND EA 5
- [SDR YENA2026020400129](https://openairdocs.org/sdr/YENA2026020400129.md): Seat Track · broken · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: BROKEN SEAT TRACK Y1292, -Y765 AND -Y1292 BOLT AT LEVEL FR47 IN PASSENGER CABIN (3EA); REF AEROMAN WO# 2025-413/1 WCC# 2025-682634 FOR WORK PERFORMED; REMOVED AND REPLACED SEAT TRACK BOLTS LOC. Y1292, -Y765 AND -Y1292 AT LEVEL FR47 I
- [SDR YENA2026020400128](https://openairdocs.org/sdr/YENA2026020400128.md): Stringer · corroded · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOC BTW FR 56 TO FR 57 IN AFT CARGO COMPARTMENT (CPCP FINDING); REF AEROMAN NR 2025-682543 WO 2025 413/1 REMOVED AND REPLACED STRINGER 43LH LOC BTW FR 54 TO FR 60 IN AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11,
- [SDR YENA2026020400127](https://openairdocs.org/sdr/YENA2026020400127.md): Structure · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CRACK FLOOR STRUCTURE UPPER SECTION CONNECTION LOC FR 66 AT LEVEL STR 23KH AT AFT GALLEY AREA (1EA); REMOVED AND REPLACED FLOOR STRUCTURE UPPER SECTION CONNECTION LOC FR 66 AT LEVEL STR 23LH SIDE AT AFT GALLEY AREA (1EA)IAW A320 SRM 5
- [SDR YENA2026020400126](https://openairdocs.org/sdr/YENA2026020400126.md): Stringer · corroded · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOC BTW FR 57 TO FR 58 IN AFT CARGO COMPARTMENT (CPCP FINDING); REF AEROMAN NR 2025-682544 WO 2025 413/1 REMOVED AND REPLACED STRINGER 43LH LOC BTW FR 54 TO FR 60 IN AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11,
- [SDR YENA2026020400125](https://openairdocs.org/sdr/YENA2026020400125.md): Stringer · corroded · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE:CORROSION STRINGER 43L LOC BTW FR 54 TO FR 56 IN AFT CARGO COMPARTMEN T (CPCP FINDING); REF AEROMAN NR 2025-682549 WO 2025 413/1 REMOVED AND REPLACED STRINGER 43LH LOC BTW FR 54 TO FR 60 IN AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11,
- [SDR YENA2026020400124](https://openairdocs.org/sdr/YENA2026020400124.md): Skin · corroded · Feb 2, 2026 · N587JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION FALSE SPAR BOX LOWER SKIN UPPER SURFACE AT LEVEL RIB 6A ON RH WING (CPCP FINDING); ACCOMPLISHED REPAIR OF CORROSION DAMAGE ON THE RH WING, BOTTOM SKIN PANEL 3 UPPER SURFACE AT LEVEL RIB 6A, FALSE SPAR BOX AREA I.A.W AEM AE
- [SDR YENA2026020400123](https://openairdocs.org/sdr/YENA2026020400123.md): Skin · corroded · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION SKIN PANEL INTERNAL STRUCTURE LOC BTW FR 16 AND 17 LOWER AREA ON LATERAL AVIONIC COMPARTMENT LT SIDE. PERFORMED PERMANENT REPAIR IAW EA# 53-0089-25, EC# A26-029-0. REPAIR IS CAT A AND NO FURTHER INSPECTION IS REQUIRED. WOR
- [SDR YENA2026020400122](https://openairdocs.org/sdr/YENA2026020400122.md): Fitting · corroded · Feb 2, 2026 · N587JB · Airbus A320232 · Nacelle/Pylon, Main Frame
  > DURING HEAVY MAINTENANCE: CORROSION ON SPIGOT LOWER FITTING ON LH PYLON; (RESOLVED ON W/O: 1420259 TASKCARD: NR-00037) REF AEROMAN NR 2025-682782 WP 2025-413/1. REMOVED AND REPLACED THE SPIGOT LOWER FITTING ON LH PYLON IAW SRM 54-51-283-002, SRM 51-44-11-801,
- [SDR YENA2026020400121](https://openairdocs.org/sdr/YENA2026020400121.md): Fitting · corroded · Feb 2, 2026 · N587JB · Airbus A320232 · Nacelle/Pylon, Main Frame
  > DURING HEAVY MAINTENANCE: CORROSION IN THE SPIGOT LOWER FITTING ON RH PYLON; (RESOLVED ON W/O: 1420259 TASKCARD: NR-00038) REF AEROMAN NR 2025-682784 WP 2025-413/1. REMOVED AND REPLACED THE SPIGOT LOWER FITTING ON RHPYLON IAW SRM 54-51-283-002, SRM 51-44-11-80
- [SDR YENA2026020400120](https://openairdocs.org/sdr/YENA2026020400120.md): Web · corroded · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE WEB LOC. BTW FR69/70 AT LEVEL STR23L AT AFT GALLEY AREA (1 EA) (CPCP FINDING); REF AEROMAN NR 2025-682631 WO 2025 413/1 REMOVED AND REPLACED FLOOR STRUCTURE WEB LOC BTW FR69 TO FR70 AT LEVEL STR23L AFT GALLEY
- [SDR YENA2026020400119](https://openairdocs.org/sdr/YENA2026020400119.md): Skin · corroded · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION SKIN PANEL INTERNAL STRUCTURE LOC BTW FR 16 AND 17 LOWER AREA ON LATERAL AVIONIC COMPARTMENT LH SIDE; PERFORMED PERMANENT REPAIR IAW EA# 53-0089-25, EC# A26-029-0. REPAIR IS CAT A AND NO FURTHER INSPECTION IS REQUIRED. WORK
- [SDR YENA2026020400118](https://openairdocs.org/sdr/YENA2026020400118.md): Skin · corroded · Feb 2, 2026 · N587JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE BOTTOM SKIN PANEL NO. 3, BTW REAR SPAR AND FA LSE REAR SPAR, AND BTW WX2825 STIFFENER DATUM AND RIB DATUM INBOARD DI AGONAL ON LH WING (CPCP FINDING); REF AEROMAN NR 2025-682418 WO 2025 413/1 CCOMPLISH REPAIR O
- [SDR YENA2026020400117](https://openairdocs.org/sdr/YENA2026020400117.md): Doubler · corroded · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / NLG COMPARTMENT REINFORCEMENT DOUBLER AT FR16-17 AND Y+250 / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEM EA 53-0089-25 REV 0 (COVER AND PARTS 1 - 5) /2/ AIRBUS RDAF 81702470/003/2025#A /3/ REPAIR I
- [SDR YENA2026020400116](https://openairdocs.org/sdr/YENA2026020400116.md): Floorbeam · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / FRONT SPAR VERTICAL STRINGERS & HORIZONTAL FLOOR BEAMS / @ LEVEL OF FR36 & Y-1292, Y-765, Y-254, Y+254, Y+765 & Y+1292 / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 57-0117-25 REV. 0 (COVER + PARTS
- [SDR YENA2026020400115](https://openairdocs.org/sdr/YENA2026020400115.md): Skin · corroded · Feb 2, 2026 · N587JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: WINGS / LH WING / BOTTOM SKIN PANEL 3 / RIBS 6A, REAR SPAR-FALSE REAR SPAR / CORROSION - TEMPORARY REPAIR; REFERENCES: /1/ AEROMAN EA 57-0122-25 COVER & PARTS 1-11 /2/ AIRBUS RDAF 81692663/023/2025 ISSUE A /3/ AIRBUS TD/81692663/012/2
- [SDR YENA2026020400114](https://openairdocs.org/sdr/YENA2026020400114.md): Pressure Deck · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / PRESSURE DECK PANEL / FR36 RHS / ATTACHMENT HOLES / CRACKS – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0085-25 REV. 0 (COVER + PARTS 1-8) /2/ AIRBUS DOSSIER 81696490 /3/ AIRBUS RDAF 81696490/003/2
- [SDR YENA2026020400113](https://openairdocs.org/sdr/YENA2026020400113.md): Window Frame · cracked · Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CTR POST LOWER NODE AREA VERTICAL FLANGE RHS & CONT. FITTING LHS / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0081-25 (COVER + PARTS 1-5) /2/ AIRBUS DOSSIER 81689336 /3/
- [SDR YENA2025041100392](https://openairdocs.org/sdr/YENA2025041100392.md): Power Supply · inoperative · Apr 6, 2025 · N587JB · Airbus A320232 · Emergency Lighting
  > FLT#460, FLL-BDL. 'EMERGENCY EXIT LIGHTS DID NOT TURN ON FOR LANDING OVER L1 & R1 DOORS; REPLACED FWD CABIN EPSU (10WL)IAW AMM 33-51-38-400-001-A, OPS CHECKS NORMAL, MCC NOTIFIED.'
- [SDR YENA2024092001285](https://openairdocs.org/sdr/YENA2024092001285.md): Warning Message · illuminated · Sep 19, 2024 · N587JB · Airbus A320232 · Emergency Lighting
  > FLT#87, ALB-FLL.' DURING CABIN EMERGENCY LIGHT TEST TASK CARD, "EPSU EXT LOAD FWD L" FAULT ON FWD FAP; ACCOMPLISHED EPSU BITE TEST PER M/M 33-51-00-710-001, OPS CHECKED NORMAL.'
- [SDR YENA2024080801094](https://openairdocs.org/sdr/YENA2024080801094.md): Apu · contaminated · Aug 6, 2024 · N587JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT#379, DCA-FLL. ' FUMES REPORTED BY INBOUND CREW, MY CREW AND MX VERIFIED; COMPLIED WITH INFO NOTICE 2017-T015 SECTION B2 IDENTIFIED ODOR COMING FROM APU, DECONTAMINATION LEVEL 2 WAS ACCOMPLISHED PER TSM 05-50-00-810-085B. AIRCRAFT IS OK FOR SERVICE.'
- [SDR YENA2024071901006](https://openairdocs.org/sdr/YENA2024071901006.md): Unknown · odor · Jul 16, 2024 · N587JB · Airbus A320232 · Air Distribution System
  > FLT#1696, SJO-MCO. 'DIRTY SOCK SMELL REPORTED BY INFLIGHT UPON ARRIVAL AT GATE. SMELL WAS ON FINAL DECENT MID AFT CABIN; COMPLIED WITH INFO NOTICE 2017-T015 SECTION B2. IDENTIFIED ODOR TRANSIENT ENVIRONMENTAL ODOR. PERFORMED "ECS" DECONTAMINATION PER TSM 05-5
- [SDR YENA2024062700917](https://openairdocs.org/sdr/YENA2024062700917.md): Landing Gear · malfunctioned · Jun 26, 2024 · N587JB · Airbus A320232 · Landing Gear Retraction/Extension System
  > FLT#305, EWR- FLL. (AIRCRAFT PERFORMED AN AIR TURN BACK). 'DURING CLIMB OUT AT 3000' LAND GEAR DOOR (NOSE) COULD BE HEARD BANGING / CLOSING REPEATEDLY NO ECAM; PERFORMED CLEARANCE CHECK ON NLG DOORS ALL WITHIN LIMITS INSPECTED ALL AVIONICS COMPARTMENT FOR POSS
- [SDR YENA2024030600356](https://openairdocs.org/sdr/YENA2024030600356.md): Wire Harness · shorted · Mar 1, 2024 · N587JB · Airbus A320232 · Engine Indicating System Wiring
  > FLT#365, BOS-RSW. (AIRCRAFT DIVERTED TO JFK). 'ENG 1 EGT INDICATION INOP. AMBER XX AFTER TAKEOFF; PER TSM 77-20-00-810-801-B. FOUND EGT HARNESS SHORTED TO GROUND REMOVED AND REPLACED ENG #1 EGT HARNESS IAW AMM 77-21-43. OPS CHECK NORMAL.'
- [SDR YENA2023110201339](https://openairdocs.org/sdr/YENA2023110201339.md): Unknown · unknown · Oct 28, 2023 · N587JB · Airbus A320232 · Emergency Lighting
  > FLT#711, JFK-LAS. 'LOWER EXIT SIGN ROW 10 WIRE EXPOSED COVER MISSING EXIT MARKING SIGNS 1) WALL MOUNTED EXIT (MARKING) SIGNS); REPLACED LIGHT ASSY PER AMM 33-51-16. THE SYSTEM OPS CHECK GOOD. SEE 3631067, ITEMS 1 (REF LP 3631066 ITEM 1 FOUND LT SIDE EPSU (1
- [SDR YENA2023110201338](https://openairdocs.org/sdr/YENA2023110201338.md): Battery · failed · Oct 28, 2023 · N587JB · Airbus A320232 · Emergency Lighting
  > FLT#948, LAS-JFK. 'REF LP 3631066, ITEM 1 FOUND LT SIDE EPSU (11WL) DEAD; REMOVED AND REPLACEDEPSU AND BATTERY. SYSTEM OPS CHECK GOOD.'
- [SDR YENA2023110201337](https://openairdocs.org/sdr/YENA2023110201337.md): Epsu · failed · Oct 28, 2023 · N587JB · Airbus A320232 · Emergency Lighting
  > FLT#948, LAS-JFK. 'REF LP 3631066, ITEM 2 FOUND RT SIDE EPSU (12WL)FAULTED; REMOVED AND REPLACED EPSU AND BATTERY. SYSTEM OP CHECK GOOD PER AMM 33-51-38.'
- [SDR YENA2023027100199](https://openairdocs.org/sdr/YENA2023027100199.md): None · none · Feb 25, 2023 · N587JB · Airbus A320232 · Air Conditioning System
  > FLT#2701, JFK-FLL. 'ON DESCENT THE F1 NOTICED A DIRTY SOCK ODOR. IT REMAINED UNTIL WE OPENED THE A/C DOOR AT GATE; COMPLIED W/INFORMATION NOTICE 2017-T015 SECTION A. ISOLATED FAULT TO TYPE 10(A) 1C PER TSM 05-50-00-810-085-B / TSM 05-50-00-810-085D. THE AIRCRA
- [SDR YENA2023024100186](https://openairdocs.org/sdr/YENA2023024100186.md): None · none · Feb 22, 2023 · N587JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE ON INTERCOSTAL FITTING AT DOOR ST OP 7 POSITION, ON OPEN FASTENER HOLE 2, CRACK DIRECTION IS 3 O'CLOCK, A T FWD GALLEY AREA (1 EA); REF TO AEROMAN WO 2023 10/1 NR 2023-50169, REMOVED AND REPLACED I
- [SDR YENA2023024100185](https://openairdocs.org/sdr/YENA2023024100185.md): None · none · Feb 22, 2023 · N587JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE ON INTERCOSTAL FITTING AT DOOR ST OP 7 POSITION, ON OPEN FASTENER HOLE 3, CRACK DIRECTION IS 3 O'CLOCK, A T FWD GALLEY AREA (1 EA); REF TO AEROMAN WO 2023 10/1 NR 2023-50170, REMOVED AND REPLACED I
- [SDR YENA2023024100184](https://openairdocs.org/sdr/YENA2023024100184.md): None · none · Feb 22, 2023 · N587JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 35 WEB LH SIDE IN FWD FACE TO PRESSURE BULK HEAD AREA AT MORE OUTBOARD AND LOWER FASTENER, CRACK DIRECTION IS 3 OCL OCK AND CRACK LENGTH IS 0.310 INCH APPROX, IN FWD CARGO COMPARTMENT; REF AEROMAN N/R 2023- 5
- [SDR YENA2023024100183](https://openairdocs.org/sdr/YENA2023024100183.md): None · none · Feb 22, 2023 · N587JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 & STGR 30L FRAME WEB HOLE / CRACK - TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2022082500817](https://openairdocs.org/sdr/YENA2022082500817.md): A/C Pack · odor · Aug 24, 2022 · N587JB · Airbus A320232 · Cabin Cooling System
  > FLT#1693, FLL-NAS. 'ON TAKEOFF STRONG ALL ZONE SMELL AFTER ODOR ISOLATION PROCEDURE WITH PACK 1 OFF SMELL SEEMED TO DISSIPATE; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A (A), ISOLATED FAULT TO TYPE 5, (A), 1, C PER TSM 05-50-00-810-B. AIRCRAFT IS OK
- [SDR YENA2022081200791](https://openairdocs.org/sdr/YENA2022081200791.md): A/C Pack · dirty · Aug 11, 2022 · N587JB · Airbus A320232 · Cabin Cooling System
  > FLT#1709, FLL-PAP. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) ' DURING CLIMB OUT AIRFLOW FROM ALL COCKPIT SOURCES STOPPED COMPLETELY. COCKPIT TEMP ROSE QUICKLY TO AN UNBEARABLE LEVEL. FLOW RETURNED APPROXIMATELY 5-7 MINUTES LATER.' (SUPPLEMENTAL TO FOLLOW)
- [SDR YENA2022012400023](https://openairdocs.org/sdr/YENA2022012400023.md): Unknown · odor · Jan 23, 2022 · N587JB · Airbus A320232 · Air Distribution System
  > FLT 995, EWR-SXM. FLIGHT ATTENDANT ADVISED ON FINAL APPROACH A "DIRTY SOCK" SMELL WAS NOTICED + EVEN AFTER WENGINE SHUTDOWN; COMPLIED WITH INFORMATION NOTICE 2017-1015 ACTION "A"(A) ISOLATOR FAULT TO TYPE 10(A) 1C PER TSM 05-50-00-810-085-B/ TASM 05-50-00-810-
- [SDR YENA2021060400353](https://openairdocs.org/sdr/YENA2021060400353.md): Actuator · leaking · Jun 3, 2021 · N587JB · Airbus A320232 · Emergency Equipment
  > FLT# 182, BNA-FLL. L1 DOOR ASSIST ACTUATOR IS LEAKING (NOT HOLDING PRESSURE). MORE INFORMATION TO FOLLOW
- [SDR YENA2020040840313](https://openairdocs.org/sdr/YENA2020040840313.md): Skin · corroded · Apr 4, 2020 · N587JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION ON INTERNAL SKIN FOUND BETWEEN FR12 AND FR13 BETWEEN STRG32 AND STRG36RH, AFFECTING THE DOOR DOUBLER (SEE REF /1/ EA). CORROSION AT BEAM ON STGR 36 HAS ALSO BEEN REPORTED AND MUST BE REPLACED; CORROSION WAS REMOVED BY BLEND

Next page: https://openairdocs.org/aircraft/N587JB/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N587JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N587JB/reports

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